| Issue |
Volume 6, 2013
Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics
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|---|---|---|
| Page(s) | 249 - 262 | |
| Section | Fault detection and control | |
| DOI | https://doi.org/10.1051/eucass/201306249 | |
| Published online | 02 December 2013 | |
A high-fidelity airbus benchmark for system fault detection and isolation and flight control law clearance
AIRBUS Operations SAS 316 Route de Bayonne, Toulouse 31060, France
This paper presents a high-fidelity generic twin engine civil aircraft model developed by Airbus for advanced flight control system research. The main features of this benchmark are described to make the reader aware of the model complexity and representativeness. It is a complete representation including the nonlinear rigid-body aircraft model with a full set of control surfaces, actuator models, sensor models, flight control laws (FCL), and pilot inputs. Two applications of this benchmark in the framework of European projects are presented: FCL clearance using optimization and advanced fault detection and diagnosis (FDD).
© Owned by the authors, published by EDP Sciences, 2013
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 2.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.